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采用非交错网格压力修正法计算不可压及可压亚、跨、超音速流动
引用本文:朱斌,蔡睿贤,蒋洪德.采用非交错网格压力修正法计算不可压及可压亚、跨、超音速流动[J].工程热物理学报,1994(3).
作者姓名:朱斌  蔡睿贤  蒋洪德
作者单位:中国科学院工程热物理研究所
摘    要:采用非交错网格压力修正法计算不可压及可压亚、跨、超音速流动朱斌,蔡睿贤,蒋洪德(中国科学院工程热物理研究所北京100080)关键词:压力修正法,亚、跨、超音速流动一、前言源于计算不可压流动的压力修正方法,由于具有计算时间短及不受马赫数限制的优点,近年...

关 键 词:压力修正法,亚、跨、超音速流动

A NON-STAGGERED PRESSURE-BASED METHOD FOR FLOW CALCULATION AT ALL SPEEDS
Zhu Bin, Cai Ruixian, Jiang Hongde.A NON-STAGGERED PRESSURE-BASED METHOD FOR FLOW CALCULATION AT ALL SPEEDS[J].Journal of Engineering Thermophysics,1994(3).
Authors:Zhu Bin  Cai Ruixian  Jiang Hongde
Abstract:A non-staggered pressure correction numerical method has been developed to calculate both incompressible and compressible flows at all speeds. The pressure oscillation is solved by a special treatment of pressure interpolation on collocated grids, with all variables being located at the center of the control volume. Both convection and diffusion terms of the governing equations are discretized with the second-order central differencing scheme. The method is verified on a number of test cases, and the results compare favourably with other numerical results.
Keywords:pressure correction  subsonic  transonic and supersonic flow    
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